PIPER ARROW IV Maintenance Manual-PA-28RT-201-PA-28RT-201T
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INTRODUCTION. This PIPER AIRCRAFT Maintenance Manual is prepared in accordance with the GAMA (General Aviation Manufacturers Association) format. This maintenance manual is divided into various Groups which enable a broad separation of contents (Chapters) within each group. The various Chapters are broken down into major systems such as Electrical Power, Flight Controls, Fuel, Landing Gear, etc. The System/Chapters are arranged more or less alphabetically rather than by precedence or importance. All System/Chapters are assigned a number, which becomes the first element of a standardized numbering system. Thus the element “32” of the number series 32-00-00 refers to the System/Chapter on “Landing Gear.” All information pertaining to the landing gear will be covered in this System/Chapter. The major System/Chapters are then broken down into Sub-System/Sections. These sections are identified by the second element of the standardized numbering system. The number “40” of the basic number series 32- 40-00 is for the “Wheels and Brakes” portion of the landing gear. The individual units within a Sub-System/Section may be identified by a third element of the standardized numbering system, such as 32-40-0l. This number could be assigned by the manufacturer to fit the coverage requirements of the publication. Example: This manual does not contain hardware callouts for installation. Hardware callouts are only indicated where a special application is required. To confirm the correct hardware used, refer to the PA-28RT-201/201T Parts Catalog P/N 761 693, and FAR 43 for proper utilization. Introduction Page - 1 December 1, 1978 1A2 PIPER AIRCRAFT PA-28RT-201 / 201T MAINTENANCE MANUAL CHAPTER/SYSTEM LANDING GEAR SUB-SYSTEMS WHEELS AND BRAKES INDIVIDUAL UNITS NOSE WHEEL REMOVAL 32-40-01
PIPER PUBLICATIONS. ELECTRONICS: AutoFlight II Service Manual = Piper P/N 761 481 Pitch Trim Service Manual = Piper P/N 753 771 AutoControl III B and Altimatic III B Service Manual = Piper P/N 753 502 Altimatic III C Service Manual = Piper P/N 761 602 79 Vero Beach Avionics Wiring Diagrams Manual = Piper P/N 761 713 AEROFICHE: PA-28RT-201/201T Parts Catalog = Piper P/N 761 693 INSPECTION: PA-28RT-201/201T Program Inspection Manual = Piper P/N 761 736 Inspection Forms = Piper P/N 230 818 Introduction Page - 3 Added: August 17, 1982 1A4 PIPER AIRCRAFT PA-28RT-201 / 201T MAINTENANCE MANUAL
AEROFICHE GRID NUMBERING AND REVISION IDENTIFICATION 1. Aer of ic he Gr id Number ing Piper has ceased production of all Aerofiche (i.e., microfiche) products. The Aerofiche grid numbers will be removed in the next complete revision. In the interim, as partial revisions occur, the Aerofiche grid numbering system may be modified, as explained below, to simplify production. Deviations from the legacy Aerofiche grid numbering system will occur when it becomes necessary to add pages to the manual and will typically take two forms: A. Inserting pages between two existing grids in the same row. When inserting two pages between the existing grids 1A8 and 1A9, the two new pages will be numbered 1A8A and 1A8B. B. Inserting pages at the end of an Aerofiche grid row. The legacy Aerofiche grid numbering system limited page numbers in a row to a maximum of 24 (i.e., row 1A would be numbered 1A1–1A24). That limit no longer applies. Accordingly, if two pages need to be added between any existing grid row end and grid row start (i.e., 1A24 and 1B1), the new pages will simply be numbered 1A25 and 1A26. 2. Identifying Re vised Ma ter ial A. Dec 1978 through 1995: Revised text and illustrations are indicated by a black vertical line along the left-hand margin of the frame, opposite revised, added or deleted material. Revision lines indicate only current revisions with changes and additions to or deletions of existing text and illustrations. Changes in capitalization, spelling, punctuation, indexing, the physical location of the material or complete page additions are not identified by revision lines. B. 2009 and later: A revision to a page is defined as a change to the text or illustrations that existed previously. Revisions, additions and deletions are identified by a vertical line (aka change bar) along the left- hand margin of the page opposite only the text or illustration that was changed. Reformatted, but otherwise unchanged, text is not identified by a change bar. Change bars in the section Tables of Contents do not indicate a change to that page, but rather that the information in the actual paragraph has changed. A change bar in the left-hand margin opposite the footer (i.e. - chapter/section/subject, page number and date), indicates that the text was unchanged but the material was relocated to a different page. Example. NO TE : Change bars are not used in the title pages. Likewise, when a publication is completely revised (i.e. - reissued), change bars will only appear in the Tables of Contents. A reference and record of the material revised is included in each chapter’s Table of Contents/Effectivity. The codes used in the effectivity columns of each chapter are defined as follows: TABLE OF CONTENTS/EFFECTIVITY CODES Original Issue: None First Revision: Revision Identification, (1R Month-Year) Second Revision: Revision Identification, (2R Month-Year) All subsequent revisions will follow with consecutive revision numbers such as 3R, 4R, etc., along with the appropriate month-year. Added Subject: Revision Identification, (A Month-Year) Introduction Page - 4 Revised: January 31, 2009 1A5 PIPER AIRCRAFT PA-28RT-201 / 201T MAINTENANCE MANUAL
The PIPER AIRCRAFT Maintenance Manual is a comprehensive guide prepared in accordance with the GAMA (General Aviation Manufacturers Association) format. It is organized into various Groups, allowing for easy navigation and separation of contents within each group.
The manual covers major systems such as Electrical Power, Flight Controls, Fuel, Landing Gear, and more. Each system or chapter is assigned a standardized numbering system for easy reference. For example, the number series 32-00-00 refers to the System/Chapter on Landing Gear, encompassing all information related to the landing gear.
Furthermore, the major System/Chapters are divided into Sub-System/Sections, identified by the second element of the standardized numbering system. For instance, the number 40 in the series 32-40-00 pertains to the Wheels and Brakes portion of the landing gear.
Individual units within a Sub-System/Section may be identified by a third element of the standardized numbering system, such as 32-40-01, as assigned by the manufacturer to fit the publication's coverage requirements.
These manuals are invaluable resources for both professional mechanics and DIY enthusiasts, providing specific information about each aircraft, including equipment installed, weight and balance information, and more. It is essential to adhere to safety precautions and seek professional assistance if there are doubts about the ability to perform the work.
Whether for motorcycles, automobiles, or airplanes, our expertise in Aviation Information Technology ensures the preservation of technical manuals. We are committed to providing certified manuals that meet the highest standards of quality and accuracy.
By purchasing this manual, you acknowledge the importance of adhering to safety guidelines and agree to hold us harmless and indemnify us from any third-party claims arising from the use of this manual. It is crucial to thoroughly familiarize yourself with the procedures before starting any work and to use the appropriate tools and equipment for precision and safety.
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PIPER ARROW IV Maintenance Manual-PA-28RT-201-PA-28RT-201T
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